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Direct measurements of wall shear stress by buried wire gages in a shock-wave boundary-layer interaction regionDetailed measurements of wall shear stress (skin friction) were made with specially developed buried wire gages in the interaction regions of a Mach 2.9 turbulent boundary layer with externally generated shocks. Separation and reattachment points inferred by these measurements support the findings of earlier experiments which used a surface oil flow technique and pitot profile measurements. The measurements further indicate that the boundary layer tends to attain significantly higher skin-friction values downstream of the interaction region as compared to upstream. Comparisons between measured wall shear stress and published results of some theoretical calculation schemes show that the general, but not detailed, behavior is predicted well by such schemes.
Document ID
19770054185
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murthy, V. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Rose, W. C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1977
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 77-691
Meeting Information
Meeting: Conference on Fluid and Plasmadynamics
Location: Albuquerque, NM
Start Date: June 27, 1977
End Date: June 29, 1977
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
77A37037
Distribution Limits
Public
Copyright
Other

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